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EN-MC65220 Magnesium vs. AISI 204 Stainless Steel

EN-MC65220 magnesium belongs to the magnesium alloys classification, while AISI 204 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is EN-MC65220 magnesium and the bottom bar is AISI 204 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 80
210 to 330
Elastic (Young's, Tensile) Modulus, GPa 44
200
Elongation at Break, % 2.2
23 to 39
Fatigue Strength, MPa 110
320 to 720
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
77
Shear Strength, MPa 150
500 to 700
Tensile Strength: Ultimate (UTS), MPa 270
730 to 1100
Tensile Strength: Yield (Proof), MPa 200
380 to 1080

Thermal Properties

Latent Heat of Fusion, J/g 340
280
Maximum Temperature: Mechanical, °C 160
850
Melting Completion (Liquidus), °C 610
1410
Melting Onset (Solidus), °C 550
1370
Specific Heat Capacity, J/kg-K 980
480
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 26
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 120
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 80
10
Density, g/cm3 1.9
7.7
Embodied Carbon, kg CO2/kg material 27
2.4
Embodied Energy, MJ/kg 210
35

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.5
240 to 250
Resilience: Unit (Modulus of Resilience), kJ/m3 450
360 to 2940
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 62
25
Strength to Weight: Axial, points 40
27 to 40
Strength to Weight: Bending, points 49
24 to 31
Thermal Diffusivity, mm2/s 61
4.1
Thermal Shock Resistance, points 17
16 to 24

Alloy Composition

Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
15 to 17
Copper (Cu), % 0.050 to 0.1
0
Iron (Fe), % 0 to 0.010
69.6 to 76.4
Magnesium (Mg), % 93.8 to 96.8
0
Manganese (Mn), % 0 to 0.15
7.0 to 9.0
Nickel (Ni), % 0 to 0.0050
1.5 to 3.0
Nitrogen (N), % 0
0.15 to 0.3
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.010
0 to 1.0
Silver (Ag), % 1.3 to 1.7
0
Sulfur (S), % 0
0 to 0.030
Unspecified Rare Earths, % 1.5 to 3.0
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.010
0